New Mars Forums

Official discussion forum of The Mars Society plus New Mars Image Server

You are not logged in.

Announcement

Announcement: This forum is accepting new registrations via email. Please see Recruiting Topic for additional information. Write newmarsmember[at_symbol]gmail.com.
  1. Index
  2. » Search
  3. » Posts by SpaceNut

#951 Re: Human missions » A Return to the Moon by the Apollo 11 50th Anniversary. » 2025-10-13 17:13:46

closing in on that magical date..
Scientists open untouched Apollo 17 lunar samples from 1972 — they may hold clues about the moon's violent origins

it is hard to believe that someone thought to let them stayed sealed until a future where science could achive other results as compared to the past.

#952 Re: Human missions » Starship is Go... » 2025-10-13 15:54:44

web view https://www.space.com/space-exploration … ch-webcast

https://www.youtube.com/watch?v=31KE1XY32SE

3fdb6f59dbb28549cc95cc71f2be9923

NASA is counting on Starship, a 400-foot-tall, super-heavy-lift rocket and spaceship system, to put its first astronauts on the moon under a $4.2 billion contract. Though the U.S. space agency has its own rocket and spaceship, Starship is expected to ferry the crew from lunar orbit to the moon's surface for the last leg of the journey.

SpaceX says refueling its Starship in space won't be scary

Why does NASA want a propellant depot in space?
NASA and commercial partners are interested in space fuel stations because they could allow spacecraft to travel longer and farther into the solar system. Future missions could use ice on the moon to make propellant by splitting water molecules into hydrogen and oxygen. If engineers can figure out how to store super-cold liquids in space, whether they are launched from Earth or produced somewhere else, it could make a long-term stay on the moon possible and even support distant missions to Mars.

NASA has invested $370 million in over a dozen U.S. companies to develop the technology needed to store and transfer rocket fuel in space. That funding includes $53 million for SpaceX to demonstrate a propellant transfer, from tanker to ship, in orbit.

The U.S. space agency has chosen to use private vendors for moon landers to buy down the technical risks and costs of the Artemis program, which seeks to use the moon as a springboard for eventual missions to Mars. SpaceX was the first selected, and Blue Origin, billionaire Jeff Bezos' rival space company, was awarded the contract for Artemis V, a crewed mission slated for no earlier than 2029.

images-3.fill.size_1400x788.v1705009837.webp

#954 Re: Human missions » Going Solar...the best solution for Mars. » 2025-10-13 15:25:23

Void in another topic was talking about alignment of solar and getting the most out of it.

futurevoltaics-vecthor-despiece-bifacial-solar-panel-reflectors.png

https://www.youtube.com/watch?v=xD1MT-ek05w
Bifacial Solar Panels are CHANGING the Game! Vertical Results Part 2

Raising a PV system’s yield by 20% with mirror reflectors

cc64250f-df86-4b0a-aad0-fbc0119026a8.jpeg

A system with vertical solar panels inside a reflective parabola, like a Compound Parabolic Concentrator (CPC), can increase energy output by concentrating sunlight onto the panels from multiple angles. While a basic parabolic reflector must be precisely aimed at the sun, a CPC is designed to collect and concentrate light over a range of angles, and a secondary reflector can be added to capture light that wouldn't otherwise reach the panels. This combination can boost efficiency, particularly for bifacial panels, by channeling more reflected and direct light to the panels and potentially mitigating losses from non-ideal angles
How it works
Parabolic Concentrator: A Compound Parabolic Concentrator (CPC) uses a reflector with a specific parabolic shape to concentrate sunlight onto a target, like a solar panel, from a wide range of angles.
Vertical Bifacial Panels: Vertical panels have the advantage of generating energy from both their front and back sides (bifacial). They also have a more even energy production curve throughout the day, peaking in the morning and evening instead of just at noon.
Synergy: Placing a CPC around the panels can increase the amount of light the panels receive. The reflector captures sunlight that might have otherwise missed the panels and directs it to them. A secondary reflector can be used to further increase the amount of light captured.
Increased Efficiency: By concentrating more light onto the panels, this configuration can significantly increase the panel's energy output, potentially much more than a simple reflector.
Benefits
Higher Energy Yield: The concentrated and reflected light increases the total energy captured by the panels.
Improved Energy Profile: Vertical panels with east-west orientation produce a more consistent power output throughout the day, which can be beneficial for matching demand curves.
Reduced Cooling: Vertical panels stay cooler than traditional panels because they are shaded at noon, which improves their efficiency.
Space Efficiency: This system is more efficient at using land area, which is a benefit in areas where space is limited.
Considerations and limitations
Complexity: The design and construction of a CPC system can be more complex and expensive than standard panel installations.
Precise Aiming: Unlike a simple reflector, a CPC is designed to work over a range of angles, but it still requires some aiming to be effective.
Maintenance: Mirrors need to be kept clean to maintain their reflectivity, which adds to the maintenance workload.
Heat Generation: Concentrating sunlight can also increase the panel's temperature, which reduces its efficiency.

#955 Re: Human missions » 40 Rocket Launches for One Moon Mission? » 2025-10-13 12:35:48

AI Overview
Block 3 Starship and Super Heavy are a planned set of upgrades focusing on significant increases to thrust, propellant capacity, and overall size. The following specifications are derived from official SpaceX announcements and reports from aerospace news outlets and fan communities.
bbcode
[size=150]Starship Block 3 Specifications[/size]

Overview
Block 3 represents a significant scale-up of the Starship architecture, with a focus on delivering a truly high-performance, fully reusable launch system. It incorporates major upgrades, including the use of Raptor V3 engines, a longer vehicle, and structural improvements.

Full Stack (Starship + Super Heavy)

  • Height: 124.4 m (408 ft)

  • Diameter: 9 m (30 ft)

  • Payload to LEO (fully reusable): Up to 100 t (220,000 lb)

  • Engines: All Raptor V3 engines across both stages.

Super Heavy Booster (Block 3)

  • Height: 72.3 m (237 ft)

  • Propellant Capacity: 3,650 t (8,050,000 lb)

  • Engines: 33 Raptor V3 engines.

  • Maximum Thrust: 80.8 MN (18,200,000 lbf).

  • Grid Fins: Reduced from four to three larger fins, integrated into the catch pins and positioned lower on the vehicle for better heat management during stage separation.

  • Hot Staging: Redesigned integrated hot staging ring with improved venting to handle the higher thrust of the Raptor V3 engines.

Starship Upper Stage (Block 3)

  • Height: 52.1 m (171 ft).

  • Propellant Capacity: 1,550 t (3,300,000 lb).

  • Engines: 6 Raptor V3 engines (3 sea-level, 3 vacuum-optimized). Future versions may include up to 9 engines.

  • Heat Shield: Features a fully reusable, metallic heat shield with built-in cooling pathways for improved reliability and mass savings.

Raptor V3 Engine

  • Thrust (Sea-level): 280 tf (507 klbf). Future versions aim for 300+ tons of thrust.

  • Engine Mass: 1,525 kg, a reduction from the V2 engine.

  • Cooling System: Integrated cooling circuits, eliminating the need for a separate heat shield on the aft of the booster.

Key Upgrades & Features

  • Increased Thrust and Payload: Raptor V3 engines provide a substantial boost in power, enabling a higher payload capacity to orbit.

  • Refined Design: A simpler, more reliable aft booster design, with components either removed or better integrated.

  • Improved Hot Staging: An integrated hot staging ring and improved venting mechanism designed for increased engine power.

  • Florida Operations: The Block 3 vehicle is compatible with the new Orbital Launch Pad at Kennedy Space Center, facilitating a higher launch cadence.

Development & Status
As of October 2025, Block 3 vehicles are in production and undergoing testing, with the final Block 2 vehicle having already flown. SpaceX aims for heavy flight activity for Block 3 in the coming year.

SpaceX Starship Block 3 specifications
Overview
Full Stack Height: ~124.4 m (408 ft)
Payload to LEO (fully reusable): 100 t, with a potential to increase to 150 t
Target Mission: Long-duration missions to the Moon and Mars
Key Improvements: Upgraded engines, simplified design, and a larger integrated hot-staging ring
Super Heavy Booster (Block 3)
Height: 72.3 m (237 ft)
Diameter: 9 m (30 ft)
Engines: 33 Raptor 3 engines
Maximum Thrust: 80.8 MN (18.2 million lbf)
Propellant Mass: 3,650 t (8.05 million lbs)
Structural Changes:
Simplified aft section and integrated hot-staging ring
Fewer, larger grid fins, integrated with the catch pins
Propellants: Liquid Methane (CH4) and Liquid Oxygen (LOX)
Starship Second Stage (Block 3)
Height: 52.1 m (171 ft)
Diameter: 9 m (30 ft)
Engines: 6 Raptor 3 engines (3 sea-level, 3 vacuum-optimized)
Maximum Thrust: 26.48 MN (5.95 million lbf)
Propellant Mass: 1,500 t (3.3 million lbs)
Structural Changes:
New integrated hot-staging system
Upgraded thermal protection system with full-stack reusability
Propellants: Liquid Methane (CH4) and Liquid Oxygen (LOX)
Raptor 3 Engines
Purpose: Powers both the Super Heavy booster and Starship upper stage
Key Features:
Higher thrust and improved efficiency
Integrated cooling circuits to eliminate the need for a separate heat shield on the engine bay
Thrust (Sea-level): 280 tf
Thrust (Vacuum-optimized): Higher than sea-level
Specific Impulse (Sea-level): 330s
Specific Impulse (Vacuum): 350

#956 Re: Terraformation » Will Mars be terraformed » 2025-10-13 12:26:33

Could we really turn Mars green?

Terraforming is the theoretical process of transforming a planet or moon to make it habitable for humans and other Earth-like life. The concept involves altering an alien world's atmosphere, temperature, and surface conditions to resemble Earth's environment, such as adding oxygen to the air, creating liquid water on the surface, and establishing a stable climate.

Mars is the most commonly discussed candidate for terraforming, with proposals ranging from releasing greenhouse gases to warm the planet, to introducing microorganisms that could gradually produce oxygen over thousands of years.

Until recently, the idea of terraforming Mars has belonged to science fiction, a grand vision of transforming the cold, barren red planet into a world teeming with life. The idea has captured imaginations for generations, but serious scientists have largely dismissed it as impossible.

In a new paper posted to the arXiv preprint server, a team of researchers led by Dr. Erika DeBenedictis from Pioneer Labs argues it's time to take terraforming seriously as a research program, not because we should start tomorrow, but because recent breakthroughs in several fields have shifted the concept from impossible to merely very difficult.

Dr. DeBenedictis, the CEO of Pioneer Labs, authored a workshop summary that was prepared for the 2025 Green Mars Workshop, makes the case plainly and simply. Thirty years ago, terraforming Mars wasn't just hard, it was impossible. But new technologies, from SpaceX's Starship potentially slashing launch costs by a factor of a thousand, to advances in synthetic biology and climate modeling, have fundamentally changed the equation. The question is no longer whether terraforming is physically possible, but whether we should even pursue it and how we might approach such an incredible undertaking.

The workshop summary presents an intriguing narrative, beginning with possible planetary endpoints and tracing back to the steps required to reach them. The vision unfolds in phases. First comes warming, raising Mars's average temperature by tens of degrees within a few decades using engineered aerosols or greenhouse gases. Recent research suggests Mars harbors enough water ice to then form an ocean covering nearly 4 million square kilometers at depths of 300 meters. A temperature increase of around 30°C could begin melting these frozen reserves, creating conditions where liquid water could exist on the surface.

The second phase involves establishing microbial life. Here's where synthetic biology becomes crucial. Researchers propose engineering extremophiles, microbes that thrive in harsh conditions, combining traits like temperature tolerance, radiation resistance, and indifference to atmospheric pressure. These hardy organisms could potentially cover Mars with algae-like growth within decades, beginning the slow process of atmospheric transformation through photosynthesis.

The final phase stretches across centuries or even millennia, building an oxygen-rich atmosphere thick enough to support complex life. The team suggests starting within enormous domed habitats, 100 meters tall, where photosynthesis or water electrolysis could generate breathable air. Beyond these structures, spreading plant life would gradually contribute oxygen to the broader atmosphere, though this natural process alone would take a thousand years. Eventually though, human explorers could leave the protective domes and live on the planet's surface.

The research also highlights critical unknowns that must be addressed. What lies beneath the extensive ice sheets on Mars? How would dust storms behave in a warmer, wetter atmosphere? Are materials needed for large-scale water electrolysis, are they abundant enough on Mars, or would they require expensive importation from Earth?

Beyond the technical challenges lie the ethical questions. If we decide to terraform Mars, we will change it in ways that may not be reversible. Mars has its own planetary history, and terraforming would effectively end our opportunity to study that pristine record. If indigenous Martian life exists, even in microbial form, our interventions could destroy it.

The researchers argue that studying terraforming has immediate practical benefits for Earth. Technologies developed for Mars habitation, from desiccation-resistant crops to sustainable closed-loop systems, could directly benefit our home planet. Developing green technologies for space might offer a pathway to maturing them for terrestrial use.

I have to confess, as a not-so-closeted space enthusiast, there's something compelling about approaching planetary engineering not as immediate action but as rigorous research. The workshop summary doesn't advocate launching terraforming missions tomorrow. Instead, it calls for careful laboratory studies, detailed climate modeling, and perhaps small-scale experiments on future Mars missions to test localized warming strategies.

But, and it's a big but, before we consider transforming an entire world, we must thoroughly understand what we're working with and what we might be risking. The conversation has shifted from "could we?" to "should we, and if so, how?" and that represents genuine, considered progress.

https://dx.doi.org/10.48550/arxiv.2510.07344

#957 Re: Human missions » 40 Rocket Launches for One Moon Mission? » 2025-10-13 12:03:58

Much of the numbers are coming from the targeted payload to orbit and what is needed for the Gateway. The later is definately not as solid.

Block 3 is the final version to target.

current-starship-2-and-starship-3s-proposed-specs-via-elons-v0-ik3pfxudgwsc1.jpeg?width=1080&crop=smart&auto=webp&s=da6be20e6755e66f7414a0667e8a8edfb86ed7a8

Starship's fully reusable cargo capacity to Low Earth Orbit (LEO) is up to 150 metric tons (330,000 lbs), with a design target of over 100 tons to Mars and the Moon. The vehicle's block design aims to increase this capacity over time, with Block 2 aiming for 100-150 tons and Block 3 targeting 200 tons. 

Capacity by Block (LEO):
Block 1: Aimed for approximately 100 tons.
Block 2: Designed to carry 100-150 tons to LEO.
Block 3: Targeted to carry up to 200 tons to LEO.

Key Factors for Capacity:
Full Reusability: The design focuses on full reusability, impacting overall capability.

The Starship Block 3 specifications include:
Height: Approximately 140 to 150 meters (461 to 492 feet).

Payload Capacity: Up to 200 tons to low Earth orbit (LEO) when fully reusable.

Engine Configuration: Equipped with 33 upgraded Raptor 3 engines.

Propellant Capacity: Increased by 25% compared to Block 2, enhancing launch capabilities.

Design Features: Includes a docking system for on-orbit refueling and a reinforced cargo bay.


These upgrades aim to support more extensive missions, including those to Mars and the Moon.
Orbital Refueling:
Starship is designed to be refueled in orbit, allowing it to carry more payload to other destinations like Mars.

Expended Configuration:
When not fully reusable, Starship is projected to carry even larger loads, potentially 250+ tons to orbit.

Cargo Configuration:
Starship can be configured for a variety of payload types and can autonomously deploy them to Earth, Lunar, or Martian surfaces.

The height of the full Starship stack, consisting of the Super Heavy booster and the Starship upper stage, varies by block, with recent versions like the Block 2 being around 404 feet (123.1 meters) tall and larger versions like Block 4 reaching approximately 466 feet (142 meters). The height of the two stages are: Block 2, the upper Starship spacecraft, is 171 feet (52.1 meters) tall, and the Super Heavy booster is 232 feet (71 meters) tall. 

Full Starship Stack Height by Block
Block 1: Approximately 398 feet (121.3 meters).
Block 2: Around 404 feet (123.1 meters).
Block 3: About 408 feet (124.4 meters).
Block 4: Approximately 466 feet (142 meters).

Component Heights
Starship spacecraft (Ship): The 171-foot upper stage.
Super Heavy booster: The 232-foot first stage.
These measurements represent the integrated launch system, not just the spacecraft or the booster alone, and are subject to change as the system continues to be developed

edit:
its about the volume shape between the blocks that means problems for the cargo we would want.
Block 1 is just 23 m tall with the internal diameter of 9 M but is the cylinder to where it arcs
Block 2 they are striving for 52 m for that same 9 m diameter.

These make and placement of moon equipment to fit a fresh design to make use of the internal volume.

#958 Human missions » 40 Rocket Launches for One Moon Mission? » 2025-10-13 09:27:11

SpaceNut
Replies: 3

40 Rocket Launches for One Moon Mission? NASA’s Wild Bet on Starship Explained

Thats more sever than we had thought...

The global race to return humans to the Moon is accelerating, and the United States is betting big on SpaceX’s colossal Starship rocket. As reported by CNNon October 12, 2025, China is advancing rapidly with its own crewed lunar mission, raising serious questions about whether NASA’s current approach can deliver results in time. The answer may hinge on a pivotal Starship test flight scheduled for Monday in South Texas.

Starship Becomes NASA’s Linchpin For Artemis
Set to serve as the Human Landing System (HLS)for the Artemis III mission, Starship is a critical component of NASA’s plan to land astronauts on the Moon by 2027. Its role is to ferry astronauts from lunar orbit to the surface and back. However, despite its towering ambition and unmatched scale, Starship remains in development and has yet to prove it can perform under mission-level demands.

So far, the rocket has flown ten times, with six flights ending in failure. The latest prototype even exploded during ground testing. The upcoming eleventh test is expected to validate major features essential to Artemis III. Without demonstrated reliability, Starship’s place in NASA’s roadmap could become increasingly fragile.

Fueling Challenges Raise Red Flags
Starship is too large to make a full round trip to the Moon and back on a single tank. To solve this, NASA and SpaceX plan to launch a refueling depot into Earth orbit, then send multiple tanker Starships filled with cryogenic propellant to top it off.

According to engineers at NASA’s Johnson Space Center, one mission could demand more than 40 tanker launches to fully fuel the depot, far beyond SpaceX’s own earlier estimate of about ten. These launches would need to occur in rapid succession to prevent fuel loss caused by boil-off, where cryogenic fuel warms and evaporates. Former NASA exploration chief Doug Loverro cautioned, “Nobody knows how efficient the transfer is going to be,” describing it as “nearly an impossible question to answer.”

Once the depot is full, the Starship HLS, equipped to support astronauts, would launch and dock with the depot before heading to lunar orbit. Meanwhile, a separate Orion spacecraft, launched by NASA’s Space Launch System (SLS), would transport the crew. The two spacecraft would rendezvous above the Moon, enabling two astronauts to descend to the surface aboard Starship and later return to Orion for the trip home.

China’s Ambitions Sharpen The Timeline
The China National Space Administration (CNSA) aims to land astronauts on the Moon by 2030, but some experts suggest it could happen sooner. Bill Nye, CEO of the Planetary Society, warned, “The China National Space Administration will almost certainly walk on the moon in the next five years.”

Acting administrator Sean Duffy pushed back against criticism during a recent town hall, declaring, “We are going to beat the Chinese to the moon.” Political pressure has mounted as well, with Senator Ted Cruz warning that any shift in strategy now could “threaten United States leadership in space.” Despite internal concerns, the agency is pushing forward.

Is Starship ready for the Moon?
While SpaceX’s Starship promises to revolutionize space travel, some experts argue it may not have been the most practical choice for a time-sensitive mission like Artemis III. Former NASA administrator Jim Bridenstine criticized the decision, stating no prior agency leader would have opted for such a complex architecture if given alternatives.

Starship was selected in 2021 during a leadership gap, largely due to its low cost and bold potential. The $2.9 billion contract was awarded after beating Blue Origin, which later rejoined the Artemis program following new congressional funding, but only for future missions.

Despite technical setbacks and scheduling concerns, SpaceX continues to receive strong institutional support thanks to its track record with NASA, notably through the Commercial Crew Program. Safety advisory member Paul Hill acknowledged that the Starship timeline is “significantly challenged” and could miss the 2027 deadline by years, yet he praised the company’s unique development model. NASA press secretary Bethany Stevens emphasized the importance of ongoing dialogue with stakeholders to keep missions on track.

Related information si contained in our Starship is Go... topic.

#959 Re: Human missions » Human Business and flight plan for mars » 2025-10-13 07:26:07

Seems so long ago that the last shuttle was used and the plan had been to reuse the pieces in Constellation.
It was the chance to get out of LEO and put man on a path back and foraward.
The first objective was the creation of a small semipermanently crewed "camp" on the lunar surface in 2005–2006.
NASA was to have launched a lunar orbiting space station in 2008–2009 to support the creation of a permanently crewed moonbase by 2009–2010.

#960 Re: Planetary transportation » Bikes on Mars? - Don't laugh! » 2025-10-13 07:12:58

You may find some infor in these as well.

Quadracycles

All-Terrain Hex-Legged Extra-Terrestrial Explorer (ATHLETE)
thefirstwalk.jpg

Topics that we had in that era are gone due to great crash.

#961 Re: Planetary transportation » Bikes on Mars? - Don't laugh! » 2025-10-13 06:55:44

NASA's Chariot: Not Your Father's Lunar Rover

wow almost 2 decades ago.
94Bhv2uDjHsDKC8VTwTqA7-282-80.jpg.webp

The specifications for Chariot were set forth as follows:

  • Chariot Spec    Earth Prototype   Lunar System

    Payload           1000 kg              3000-6000 kg

    Vehicle Mass    2000 kg              1000 kg

    Top Speed        20 kph                20 kph

    Range              25 km                100 km

    Slope Climbing  15 Degrees         25 Degrees

#962 Re: Planetary transportation » Bikes on Mars? - Don't laugh! » 2025-10-13 06:49:16

Welcome back quasar777, long time....

I think you are talking about the chariot concepts.

AI Overview
NASA has funded the development of a concept for a "standing torso suit quadricycle for the moon" through a project called Chariot. Developed by a team at the Johnson Space Center, the Chariot is a multipurpose, modular lunar vehicle designed for astronauts to drive in a standing position, which gives it a "chariot-like" appearance.
Key features of the Chariot concept
Standing operation: The vehicle is specifically designed for astronauts to operate while standing, which allows them to explore more comfortably in their bulky spacesuits.
Modular design: The base mobility unit (chassis, wheels, batteries, and electronics) can be reconfigured with different attachments. These configurations allow it to serve multiple functions, such as transporting cargo, moving lunar soil (regolith), or carrying crew.
Hybrid operation: The Chariot is capable of multiple modes of control:
Onboard manual control: Direct operation by an astronaut on the vehicle.
Teleoperation: Remote control with small time delays from a lander or lunar habitation module.
Supervised autonomous control: Controlled from Earth with longer time delays.
Enhanced mobility: The standing position is intended to improve mobility for astronauts who are otherwise limited by the bulkiness of their spacesuits.
Broader lunar rover context
The standing torso suit quadricycle, or Chariot, is part of a larger effort to expand lunar mobility capabilities for the Artemis missions and beyond.
Replacing the original LRV: Like the Apollo-era Lunar Roving Vehicle (LRV), the Chariot is an unpressurized rover that will greatly expand astronauts' range and increase scientific productivity on the moon.
Supporting future exploration: In addition to crewed transportation, the Chariot is being developed to support cargo transport and other scientific objectives, including exploration of the lunar South Pole.
Complementing other vehicle designs: Other companies, such as Intuitive Machines and Lockheed Martin, are also developing unpressurized lunar terrain vehicles (LTVs). NASA has awarded contracts for the development and testing of several LTV concepts, ensuring a robust set of options for future lunar mission

#963 Re: Human missions » Starship is Go... » 2025-10-12 14:59:15

SpaceX plans to launch 11th Starship test flight in Texas as early as Monday

SpaceX said in a statement that the launch window will open at 6:15 p.m. CDT on Monday as the rocket prepares to launch from the company's Starbase compound in Texas.

SpaceX revealed that the booster used for the upcoming flight previously flew during the eighth test flight. It will lift off with 24 reused Raptor engines and attempt to land in the Gulf of Mexico rather than return to the launch site.

The primary test objective of this launch, SpaceX said, is to demonstrate a unique landing burn engine configuration planned to be used on the next generation Super Heavy rocket.

During the descent, SpaceX plans to fire 13 engines at the start of the landing burn before switching to five to steer the rocket. That's more than the three engines used in earlier tests. The new setup is meant to give the rocket more control and serve as a backup if any engines shut down.

5ebe2aec4b3de337739c5c1278ea5e73

#964 Re: Human missions » Starship is Go... » 2025-10-12 10:21:17

tahanson43206 wrote:

For Space re Post #2216...

https://newmars.com/forums/viewtopic.ph … 28#p234828

What was your source for the post?  That was NOT a quote form GW Johnson.  The header above the post implies it was.

(th)

AI generated is centaur rocket stage human rated and even when reviewed again a respose might not generate the same answer.

co pilot generate

Yes, the Centaur upper stage has been human-rated for specific missions, notably as part of NASA’s Commercial Crew Program with the Atlas V rocket.

The Centaur upper stage, developed by United Launch Alliance (ULA), has a long history of use in launching satellites and interplanetary probes. For human spaceflight, however, it required significant modifications and rigorous certification to meet NASA’s safety standards.

?? Human-Rating the Centaur for Crew Missions
NASA’s Commercial Crew Program required launch vehicles to be human-rated to safely carry astronauts to the International Space Station (ISS).

ULA adapted the Atlas V rocket with the Centaur upper stage to support Boeing’s CST-100 Starliner capsule. This configuration underwent extensive review and testing to meet NASA’s NASA-STD-8719.26 human-rating standards.

Key upgrades included:

Redundant systems for propulsion and avionics.

Enhanced structural integrity to withstand crewed launch dynamics.

Safety protocols for abort scenarios and crew protection.

? Shuttle-Centaur Legacy and Safety Concerns
In the 1980s, NASA explored using a Shuttle-Centaur configuration to launch heavy payloads like the Galileo and Ulysses probes. This version of Centaur was designed to be carried inside the Space Shuttle and deployed in orbit.

However, after the Challenger disaster in 1986, concerns about the risks of carrying cryogenic fuel inside the Shuttle led to the cancellation of Shuttle-Centaur missions. This highlighted the challenges of human-rating high-energy upper stages.

?️ What Human-Rating Really Means
Human-rating involves more than just reliability—it includes designing for crew survivability, fault tolerance, and mission assurance.

The Centaur’s adaptation for crewed missions reflects a broader shift in spaceflight toward reusable, modular, and safety-focused systems.

If you're curious about how Centaur compares to other human-rated upper stages or want to explore its role in future missions, I’d be happy to dive deeper.

AI Overview
Space tugs can use a variety of fuels, including liquid hydrogen and liquid oxygen for high-efficiency chemical engines, non-toxic "green" propellants like nitrous oxide for smaller thrusters, and propellants for electric propulsion like xenon or argon. Nuclear thermal propulsion uses a liquid propellant, most often hydrogen, heated by a nuclear reactor to generate thrust, and some high-efficiency systems use propellants like hydrogen and oxygen for power generation.
Chemical propulsion

Liquid hydrogen/liquid oxygen:
A very efficient option for high-thrust chemical rockets, though liquid hydrogen is difficult to store long-term due to "boil-off".

RP-1 (kerosene), hydrazine, or nitrogen tetroxide (NTO):
These are less efficient than liquid hydrogen/oxygen but are "earth-storable" and don't suffer from the same long-term boil-off issues.

Green propellants:
Non-toxic alternatives to hydrazine are being developed, such as nitrous oxide-based fuels, which are used in smaller thrusters on some space tugs.

Electric and nuclear propulsion Nuclear thermal propulsion (NTP):
This concept uses a nuclear reactor to heat a liquid propellant (like hydrogen) to a very high temperature and expel it through a nozzle at high velocity, providing high thrust and efficiency.

Electric propulsion:
These thrusters are highly fuel-efficient but produce very low thrust, making them suitable for long, slow maneuvers rather than rapid changes in velocity. Examples of propellants include xenon, argon, or even bismuth.

Fuel cells:
Hydrogen and oxygen can be used in fuel cells to generate electricity for other onboard systems, which can then be used by electric propulsion or other equipment

#965 Re: Human missions » Starship is Go... » 2025-10-12 07:14:22

Minimal landers would be label it a sorty mission with little act of being of permanance. What ever Nasa does needs to hold that as its primary mission in the steps to make a path for mans outward journey to the stars eventually but to planets along the way.

Using the Starship as a lifter means altering the items we have to fit a new form and fit to use it for orbital assembly. It is limited with the starship specifications listed in post #2214 above.

It might be easier to alter the starship to being a disposable second stage with new items attached at that point.

GW's space tug

A Centaur space tug is a modern adaptation of the Centaur rocket upper stage, designed to serve as a versatile in-space vehicle for transporting payloads to various destinations. Its design leverages the heritage of the Centaur stage, which has a long history as a high-energy, high-performance rocket component.

The newest version, Centaur V, is the upper stage for United Launch Alliance's (ULA) Vulcan rocket and incorporates significant upgrades for greater performance and endurance. Core design features High-energy cryogenic propellants: Centaur uses liquid hydrogen (\(LH_{2}\)) and liquid oxygen (\(LO_{2}\)) as propellants. This combination provides a high specific impulse, making it highly efficient for missions requiring significant changes in velocity (delta-v), such as moving from low Earth orbit (LEO) to geosynchronous orbit (GEO) or on interplanetary trajectories.

RL10 engines:
The stage is powered by highly reliable RL10 engines, originally developed by Pratt & Whitney and now by Aerojet Rocketdyne. The number of engines can vary; for example, the Atlas V used single-engine (SEC) or dual-engine (DEC) Centaur variants, while the Centaur V on Vulcan uses two RL10 engines.

Restart capability:
Centaur engines are designed to be restarted in space. This feature is crucial for complex missions that require multiple burns to achieve the final desired orbit or trajectory, such as deploying a payload in a geosynchronous transfer orbit and later circularizing the orbit.

Pressure-stabilized structure:
A defining characteristic of the Centaur is its thin-walled, stainless-steel structure. The tanks maintain their structural rigidity through internal pressurization from the propellants and inert gas, essentially functioning as a "steel balloon." This design reduces the stage's overall weight, maximizing the performance-to-weight ratio.

Common bulkhead:
The Centaur's liquid oxygen and liquid hydrogen tanks are separated by a common, insulated bulkhead. This design further improves mass efficiency but requires precise engineering to maintain thermal separation between the cryogenic propellants. 

Centaur V enhancements 
The latest Centaur V, developed by ULA for the Vulcan rocket, includes several upgrades that allow it to act as a more capable space tug compared to its predecessors. 

Increased energy and endurance:
The Centaur V offers 2.5 times the energy and 450 times the endurance of the older Common Centaur, allowing for more complex maneuvers and longer mission durations.

Enhanced electronics and subsystems:
The vacuum-tube-based avionics have been replaced with a modern, fault-tolerant solid-state system. Electromechanical actuators also replace the older hydraulic system for engine steering.

Larger diameter:
The Centaur V was developed by bringing forward design elements from the canceled Advanced Cryogenic Evolved Stage (ACES) program, including a wider 5.4-meter diameter. This increases propellant capacity and allows for larger payloads. 

Space tug applications 
The Centaur's advanced capabilities make it suitable for a variety of "space tug" missions beyond simply acting as a rocket's final stage. 

Interplanetary missions:
For decades, Centaur stages have launched probes to every planet in the solar system and beyond, including the Surveyor lunar landers, Voyager probes, and New Horizons.

Satellite delivery:
Centaur can deliver communications, navigation, and national security satellites directly into their final orbits, such as geosynchronous orbit, after being deployed into a lower orbit by a larger launch vehicle.

Multi-manifesting:
The endurance and restartability of the modern Centaur V allow it to deploy multiple satellites into different orbits on the same mission, which can enable more cost-effective launches for rideshare customers.

In-space logistics:
In addition to transporting payloads, Centaur can be adapted for tasks like reboosting platforms, storing and transferring propellants to other vehicles, and conducting independent scientific missions. Historical context The concept of a Centaur-derived space tug has been explored for decades. Studies in the 1970s and 1980s proposed using a reusable Centaur with the Space Shuttle, though this was canceled for safety reasons after the Challenger disaster. Nevertheless, the heritage, high performance, and continuous evolution of the Centaur design solidify its role as a premier high-energy upper stage and space tug

#966 Re: Meta New Mars » Housekeeping » 2025-10-12 07:06:30

From the idex this morning here is the trend of new posts

Meta New Mars (New post) made in: Recruiting expertise for NewMars Forum topics:

Martian Politics and Economy (New Post) made in: Martian Calender - I have created a martian calender.

Science, Technology, and Astronomy (New Post) made in: Google Meet Collaboration - Meetings Plus Followup Discussion and in OpenFOAM

Of course a program that trools the forum and then updates the NewMars home page for whats being discussed might be a feature to add so others see what is being discussed. Nasa spaceFlight has such a side bar for its forum.

#968 Re: Meta New Mars » Housekeeping » 2025-10-11 14:10:20

here is the program method to get posts from a specific user text"https://newmars.com/forums/search.php?action=show_user_posts&user_id=916"text where the user id is the number on the end

#969 Re: Business Proposals » Business Opportunity Harness Tides on Earth and elsewhere » 2025-10-10 15:40:31

1. vertical rise and fall does go slow so the capture the energy from this is simular to that of the cokoo clock weight as but in reverse. This is the bouy style floating unit using the bouyancy mass against that of the oceans water that is under it as the rise is the potential that can be created.

2. the flow of the water into inland tide rivers uses the streams flow rate to move the wheel style collection but floats of the mean ocean level.

3 wave delta are on the mean low of the tide as it rise and fall but the device lifts with the wave or is pushed by the movement of mass of the wave that slams against the device.

4. is a wave presurization chamber that could be coupled to windmill or other methods that could use air compression.

#970 Re: Science, Technology, and Astronomy » Tide Tides Tidal Energy Storage and Delivery » 2025-10-10 15:39:28

1. vertical rise and fall does go slow so the capture the energy from this is simular to that of the cokoo clock weight as but in reverse. This is the bouy style floating unit using the bouyancy mass against that of the oceans water that is under it as the rise is the potential that can be created.

2. the flow of the water into inland tide rivers uses the streams flow rate to move the wheel style collection but floats of the mean ocean level.

3 wave delta are on the mean low of the tide as it rise and fall but the device lifts with the wave or is pushed by the movement of mass of the wave that slams against the device.


4. is a wave presurization chamber that could be coupled to windmill or other methods that could use air compression.

#971 Re: Human missions » Why Artemis is “better” than Apollo. » 2025-10-09 17:26:47

Artemis II is finally set to depart Earth by April of 2026. It will bring four astronauts to the moon for a 10-day mission. The goal is to do a lunar flyby to test the Orion spacecraft and make sure it is functioning optimally and potentially address any issues that might come up. This work is critical to build on the foundation for future Artemis missions, ensuring future safety and success.

Artemis III. Right now the goal is a mid-2027 launch. It will be another crew of four, but this time, the mission will last about a month and the crew will land on the moon. They will be going to the South Pole region of the moon and stay there for about a week.

#972 Re: Business Proposals » Business Opportunity Harness Tides on Earth and elsewhere » 2025-10-09 17:16:33

Blue power: Will ocean waves be California’s new source of clean energy?

?url=http%3A%2F%2Fnpr-brightspot.s3.amazonaws.com%2F8b%2F06%2F783ddeb449858f5edc0b82ced42f%2Fecowavepower-cm-01.jpeg

Only a few small demonstration projects off the West Coast have harnessed the power of waves and tides. Costs are high and hurdles are challenging.

Some believe but the highest cost is the land and regulations.

What Is Wave Power?

oscillating-water-column-wave-energy-converter-diagram.webp

#973 Re: Business Proposals » Business Opportunity Harness Tides on Earth and elsewhere » 2025-10-08 17:26:18

Here is a post from the gravity energy storage.

was thinking about how to fill the 5 gallon pale quickly and in a flush, it came to me in that a toilet tank is a quick exit of store water just waiting to go so since I need the water to fill the pale quickly that should work to do just that. Since I wanted to have multiple pales filling with separation it will then need adequate time to refill that toilet tank to be ready for its next use. The same mechanical float and valve can be used.

Depending on the count of fill ups I might need to build up a reserve area ahead to feed that tank from the well with a more powerful pump system since it's got to get to the height to enter into the generating systems pale for use.

Now to understand the time it would take to travel down the hill for the given distance.

Normally that is the water flowing into the turbine inlet pipe or in the water wheel.
https://www.calculatoratoz.com/en/flow- … calc-28554

https://www.waterprofessionals.com/lear … alculator/

V = 0.408 × Q/D2
V = Water Velocity; Q = Flow Rate; D = Pipe Diameter

https://www.askaprepper.com/homemade-wa … -generator

Overshot-Water-Wheel.jpg

Usually, for a water wheel electric generator you need at least 3 feet of fall and at least 20 gallons per minute of flow. The more fall and flow you have, the more potential power you can generate.  You can measure flow by building a weir in the creek and measuring how fast it will fill up a 5 gallon bucket.

Power Output in kilowatts-hour is calculated by the formula: KW = 0.004 x Q x V x H x C  where:
Q = Weight of water (volume per sec x capacity of the buckets)
V = Velocity of the stream per second (meters)
H = Head, or height difference of water between the lip of the flume (head race) and the tailrace – meters
C = Efficiency Constant – usually around 50%

This is how you can actually calculate the energy your water wheel electric generator will produce.

While the flow is the travel of the pale down the hill it's the same quantity used in just part of the rotation.

Waterwheel-01-anim-525-W.gif

The 5-foot diameter water wheel shown can be scaled up or down.  The surface speed of rivers varies between about 3-8 MPH.  Floating water wheels are typically 25-45% efficient, however the pontoons shown are shaped like airfoils to increase the speed of the water between the pontoons under the wheel to increase the efficiency. 

      The water wheel turns at approximately 15-20 RPM.  The water wheel can make use of a new style generator developed for small windmills that can operate as slow as 80 RPM.  The required speed increase can be done first with a chain drive and then a belt-and-pulley system shown, or gearbox.

https://sites.google.com/site/denergysy … electrical

background.jpg

#975 Re: Business Proposals » Business Opportunity Harness Tides on Earth and elsewhere » 2025-10-07 16:46:08

Ocean-warming-is-making-big-waves-more-powerful-730x410.jpg

This metric, called wave power, has been increasing in direct association with historical warming of the ocean surface. The upper ocean warming, measured as a rising trend in sea-surface temperatures, has influenced wind patterns globally, and this, in turn, is making ocean waves stronger. Ocean Warming is Making Waves Much More Powerful University of California researchers found wave power increased globally by 0.4% every year since 1948.

Global warming is fueling stronger ocean waves

  1. Index
  2. » Search
  3. » Posts by SpaceNut

Board footer

Powered by FluxBB